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JPS63159625A - Turbo-caterpillar engine - Google Patents

Turbo-caterpillar engine

Info

Publication number
JPS63159625A
JPS63159625A JP30749686A JP30749686A JPS63159625A JP S63159625 A JPS63159625 A JP S63159625A JP 30749686 A JP30749686 A JP 30749686A JP 30749686 A JP30749686 A JP 30749686A JP S63159625 A JPS63159625 A JP S63159625A
Authority
JP
Japan
Prior art keywords
turbo
engine
many
caterpillar
shafts
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP30749686A
Other languages
Japanese (ja)
Inventor
Nobuyuki Osako
大迫　信幸
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to JP30749686A priority Critical patent/JPS63159625A/en
Publication of JPS63159625A publication Critical patent/JPS63159625A/en
Pending legal-status Critical Current

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  • Supercharger (AREA)

Abstract

PURPOSE:To improve the energy conversion efficiency of a turbo-engine by providing a caterpillar device receiving the combustion gas of the turbo-engine end extracting the kinetic energy from many shafts attached to the caterpillar device. CONSTITUTION:The high-temperature compressed air jetted from a turbo-engine 1 is received by many blades 5 arranged in a cylinder 2. The energy of the high-temperature compressed gas received by many blades 5 is transmitted to many power transmitting shafts 3 via a belt 4. Thereby, the rotating power is obtained from many power transmitting shafts 3. Accordingly, the energy conversion efficiency of the turbo-engine 1 can be improved.

Description

【発明の詳細な説明】 （Ｉ）産業上の利用分野 この発明は、燃焼ガスを受け取るキャタピラ装置を取り
つけ、キャタピラ装置に付属する数個の軸から運動エネ
ルギーを取り出せるようにしたエンジンに関する。DETAILED DESCRIPTION OF THE INVENTION (I) Field of Industrial Application The present invention relates to an engine equipped with a caterpillar arrangement for receiving combustion gases, so that kinetic energy can be extracted from several shafts attached to the caterpillar arrangement.

（ＩＩ）従来の技術 ターボプロップエンジンにおいては、１機のタービンで
燃焼ガスのエネルギーを取り出していたため、エネルギ
変換効率が低かった。(II) Conventional technology In turboprop engines, energy from combustion gas was extracted using one turbine, resulting in low energy conversion efficiency.

（ＩＩＩ）発明が解決しようとする問題点この発明はキ
ャタピラの羽根により燃焼ガスを受け、多数の軸から運
動エネルギーを得ることを目的とする。(III) Problems to be Solved by the Invention The object of the invention is to receive combustion gas by the blades of a caterpillar and to obtain kinetic energy from multiple shafts.

（ＩＶ）問題を解決するための手段 この発明をターボキャタピラエンジンとして実施した実
施例を図示にもとずいて説明すれば次の通りである。(IV) Means for Solving the Problems An embodiment in which the present invention is implemented as a turbo caterpillar engine will be described below with reference to the drawings.

第１図示のものはターボエンジン１から噴出された圧縮
高温ガスを羽根５が受け、ベルト４を通じて多数の動力
伝動軸から一定の回転を得ることが可能に構成されてあ
る。The one shown in the first figure is configured such that blades 5 receive compressed high-temperature gas ejected from a turbo engine 1, and constant rotation can be obtained from a large number of power transmission shafts through a belt 4.

（Ｖ）作用 多数の動力伝動軸３からターボエンジン１の圧縮高温ガ
スから一定の動力が得られることが可能になる。(V) Effect A constant power can be obtained from the compressed high-temperature gas of the turbo engine 1 from a large number of power transmission shafts 3.

（ＶＩ）発明の効果 この発明は以上に説明したように燃焼ガスをキャタピラ
の羽根で受け多数の軸で運動エネルギーを一定の速度で
得られる効果がある。(VI) Effects of the Invention As explained above, the present invention has the effect that combustion gas is received by the caterpillar blades and kinetic energy can be obtained at a constant speed by a large number of shafts.

そのためエネルギー変換効率が増加される。Energy conversion efficiency is therefore increased.

【図面の簡単な説明】[Brief explanation of the drawing]

図はこのターボキャタピラエンジンの実施例の１部切断
面である。The figure is a partial cross-section of an embodiment of this turbo caterpillar engine.

Claims (1)

【特許請求の範囲】[Claims] 燃焼ガスを受け取るキャタピラ装置を取り付けたキャタ
ピラエンジン。A caterpillar engine fitted with a caterpillar device that receives combustion gases.
JP30749686A 1986-12-23 1986-12-23 Turbo-caterpillar engine Pending JPS63159625A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP30749686A JPS63159625A (en) 1986-12-23 1986-12-23 Turbo-caterpillar engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP30749686A JPS63159625A (en) 1986-12-23 1986-12-23 Turbo-caterpillar engine

Publications (1)

Publication Number Publication Date
JPS63159625A true JPS63159625A (en) 1988-07-02

Family

ID=17969784

Family Applications (1)

Application Number Title Priority Date Filing Date
JP30749686A Pending JPS63159625A (en) 1986-12-23 1986-12-23 Turbo-caterpillar engine

Country Status (1)

Country Link
JP (1) JPS63159625A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013179301A2 (en) * 2012-05-29 2013-12-05 Vidhyasagar Lappasi Sundararajan Conveyor belt converted, closed work space, valved, exhaust gas evacuating, gas turbine embodiments

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013179301A2 (en) * 2012-05-29 2013-12-05 Vidhyasagar Lappasi Sundararajan Conveyor belt converted, closed work space, valved, exhaust gas evacuating, gas turbine embodiments
WO2013179301A3 (en) * 2012-05-29 2014-01-16 Vidhyasagar Lappasi Sundararajan Gas turbine

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